Memory

The -updated Lagrange formulation

Deformations (i.e. the incremental deformation matrix $F$) refers to the previous time point. TOCHNOG decomposes the incremental deformation tensor with a polar decomposition into $F = R U$ with $F$ the incremental deformation matrix, $R$ the incremental rotation matrix and $U$ the incremental stretch matrix. The incremental stretch matrix $U$ is used to determine the incremental strain matrix $0.5(U+U^T)-I$ with $I$ the identity tensor. The velocities between the two time points are the unknowns to be solved. Stresses are calculated by adding incremental stresses to the old stresses. Incremental stresses are caused by the incremental strain matrix and a rigid body rotation by the incremental rotation matrix of the old stresses.

The -updated_with_rotation Lagrange formulation

Deformations (i.e. the incremental deformation matrix $F$) refers to the previous time point. TOCHNOG decomposes the incremental deformation tensor with a polar decomposition into $F = R U$ with $F$ the incremental deformation matrix, $R$ the incremental rotation matrix and $U$ the incremental stretch matrix. The linear engineering strains in the deformed configuration are used as incremental strain matrix $0.5(F+F^T)-I$. The velocities between the two time points are the unknowns to be solved. Stresses are calculated by adding incremental stresses to the old stresses. Incremental stresses are caused by the incremental strain matrix and a rigid body rotation by the incremental rotation matrix of the old stresses.

The -updated_linear Lagrange formulation

Deformations (i.e. the incremental deformation matrix $F$) refers to the previous time point. Any rigid body rotation between the two time points are neglected, so TOCHNOG decomposes the incremental deformation tensor with a polar decomposition into $F = U$ with $F$ the incremental deformation matrix, and $U$ the incremental stretch matrix. The linear engineering strains in the deformed configuration are used as incremental strain matrix $0.5(F+F^T)-I$. The velocities between the two time points are the unknowns to be solved. Stresses are calculated by adding incremental stresses to the old stresses. Incremental stresses are caused by the incremental strain matrix.

The -total Lagrange formulation

Deformations (i.e. the total deformation matrix $F$) refers to the time 0. TOCHNOG decomposes the total deformation tensor with a polar decomposition into $F = R U$ with $F$ the total deformation matrix, $R$ the total rotation matrix and $U$ the total stretch matrix. The total stretch matrix $U$ is used to determine the total strain matrix $0.5(U+U^T)-I$ with $I$ the identity tensor. The displacements between the current time and time 0 are the unknowns to be solved. Stresses are calculated from the total displacements.

The -total_piola Lagrange formulation

Deformations (i.e. the total deformation matrix $F$) refers to the time 0. TOCHNOG decomposes the total deformation tensor with a polar decomposition into $F = R U$ with $F$ the total deformation matrix, $R$ the total rotation matrix and $U$ the total stretch matrix. The total stretch matrix $U$ is used to determine the total Green-Lagrange strain matrix $0.5 ( F^T F - I ) = 0.5 ( U^T U - I )$ Stresses are calculated from the total displacements.

The -total_linear Lagrange formulation

Deformations (i.e. the total deformation matrix $F$) refers to the time 0. TOCHNOG neglects any rigid body rotations and uses linear engineering strains $0.5(F+F^T)-I$. The displacements between the time current time and time 0 are the unknowns to be solved. Stresses are calculated from the total displacements.

See also group_materi_memory.